|
gptkbp:instance_of
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:air_traffic_control
|
digital fly-by-wire
|
|
gptkbp:collaboration
|
NASA, Roscosmos, ESA
|
|
gptkbp:communication_system
|
S-band
|
|
gptkbp:cooling_system
|
active thermal control
|
|
gptkbp:crew
|
gptkb:Andrew_R._Morgan
gptkb:Soyuz_MS-15_descent_module
gptkb:Jessica_Meir
gptkb:Oleg_Skripochka
gptkb:launch_escape_system
ongoing during mission
extensive pre-flight training
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:data_return
|
parachute landing
|
|
gptkbp:date
|
April 17, 2020
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:first_flight
|
gptkb:Soyuz_MS-16
gptkb:Soyuz_1
|
|
gptkbp:historical_significance
|
part of long-duration ISS missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-15 orbital module
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
07:16 UTC
|
|
gptkbp:launch_date
|
12:57 UTC
November 2, 2019
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:launch_window
|
limited to specific dates
|
|
gptkbp:launched
|
gptkb:Soyuz-2.1b
|
|
gptkbp:legacy
|
contributed to human spaceflight advancements
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:media_coverage
|
extensive during launch and landing
|
|
gptkbp:mission
|
transport crew to ISS
conducted by mission control
involves medical checks
|
|
gptkbp:mission_duration
|
approximately 185 days
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:operational_history
|
successfully completed missions
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:part_of
|
Soyuz MS-15 mission
|
|
gptkbp:payload_capacity
|
up to 500 kg
|
|
gptkbp:powers
|
28 V
|
|
gptkbp:propulsion
|
hypergolic thrusters
|
|
gptkbp:public_interest
|
high due to crew diversity
|
|
gptkbp:recovery_method
|
gptkb:Kazakhstan
|
|
gptkbp:research
|
conducted during ISS stay
|
|
gptkbp:safety_features
|
multiple redundant systems
|
|
gptkbp:service
|
Soyuz MS-15 service module
|
|
gptkbp:specification
|
detailed in mission reports
|
|
gptkbp:speed
|
gptkb:Soyuz_MS-15_descent_module
28,000 km/h
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-16
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_MS-15_descent_module
|
|
gptkbp:bfsLayer
|
6
|